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7108A Aluminum vs. N08800 Stainless Steel

7108A aluminum belongs to the aluminum alloys classification, while N08800 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 7108A aluminum and the bottom bar is N08800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 11 to 13
4.5 to 34
Fatigue Strength, MPa 120 to 130
150 to 390
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 210
340 to 580
Tensile Strength: Ultimate (UTS), MPa 350
500 to 1000
Tensile Strength: Yield (Proof), MPa 290 to 300
190 to 830

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 210
1100
Melting Completion (Liquidus), °C 630
1390
Melting Onset (Solidus), °C 520
1360
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 150
12
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
30
Density, g/cm3 2.9
8.0
Embodied Carbon, kg CO2/kg material 8.3
5.3
Embodied Energy, MJ/kg 150
76
Embodied Water, L/kg 1150
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 38 to 44
42 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 610 to 640
96 to 1740
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 33 to 34
18 to 35
Strength to Weight: Bending, points 38
18 to 28
Thermal Diffusivity, mm2/s 59
3.0
Thermal Shock Resistance, points 15 to 16
13 to 25

Alloy Composition

Aluminum (Al), % 91.6 to 94.4
0.15 to 0.6
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.040
19 to 23
Copper (Cu), % 0 to 0.050
0 to 0.75
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.3
39.5 to 50.7
Magnesium (Mg), % 0.7 to 1.5
0
Manganese (Mn), % 0 to 0.050
0 to 1.5
Nickel (Ni), % 0
30 to 35
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.030
0.15 to 0.6
Zinc (Zn), % 4.8 to 5.8
0
Zirconium (Zr), % 0.15 to 0.25
0
Residuals, % 0 to 0.15
0